System and methods for airborne launch and recovery of aircraft

Abstract

A system and methods for airborne launch and recovery of aircraft. In one embodiment the system comprises a flexible tether configured to be towed behind an airborne mother ship. A drag device is secured to a distal end of the flexible tether to generate drag and maintain tension in the flexible tether. A reel associated with the mother ship anchors a proximal portion of the flexible tether and selectively lets out and takes up the flexible tether to adjust a length of the flexible tether. A capture mechanism associated with the aircraft engages the flexible tether to enable the aircraft to translate along the flexible tether. In embodiments of the present methods, a flexible tether is deployed from an airborne mother ship. An aircraft translates forward and rearward along the flexible tether. Prior to launch, the weight of the aircraft is transferred from the flexible tether to the wings. During recovery, the weight of the aircraft is transferred from the wings to the flexible tether.

Description

BACKGROUND[0001]1. Technical Field[0002]The present disclosure relates to aircraft.[0003]2. Description of Related Art[0004]In modern warfare tactical aircraft are an indispensable asset to military commanders. However, tactical aircraft are limited by, for example, fuel capacity, weaponry capacity and configuration, and maintenance intervals. In-flight refueling can extend combat operations. However, aircraft must still return to a ground base to rearm and to have maintenance performed. Similarly aircraft used in civilian applications such as crop-dusting, aerial police / traffic surveillance, and countering man-portable air-defense systems are also limited by their need to return to ground for maintenance, reconfiguration, etc.[0005]These limitations are exacerbated in unmanned air vehicles (UAVs) and unmanned combat air vehicles (UCAVs). For simplicity, the abbreviation UAV will be used herein to refer to both unmanned air vehicles and unmanned combat air vehicles. With the advent ...

AI Technical Summary

Benefits of technology

[0008]The embodiments of the present system and methods for airborne launch and recovery of aircraft have several features, no single one of which is solely responsible for their desirable attributes. Without limiting the scope of the present embodiments as expressed by the claims that follow, their more prominent features will now be discussed briefly. After considering this discussion, and particularly after reading the section entitled “Detailed Description”, one will understand how the features of the present embodiments provide advantages, which include the ability to recover and re-launch aircraft so that their missions can be extended indefinitely, and the ability to recover and launch aircraft smoothly without being significantly affected by turbulent airflow near the mother ship.

[0009]One aspect of the present embodiments includes the realization that it would be advantageous to be able to launch and recapture aircraft, such as UCAVs, from an airborne mother ship. The ability to recapture the aircraft would advantageously enable refueling, re-supplying, rearming and / or reconfiguration of the aircraft in flight, during the course of a mission. Such capabilities would enable the mission of each such aircraft to be extended indefinitely.

Problems solved by technology

However, tactical aircraft are limited by, for example, fuel capacity, weaponry capacity and configuration, and maintenance intervals.

Similarly aircraft used in civilian applications such as crop-dusting, aerial police / traffic surveillance, and countering man-portable air-defense systems are also limited by their need to return to ground for maintenance, reconfiguration, etc.

These limitations are exacerbated in unmanned air vehicles (UAVs) and unmanned combat air vehicles (UCAVs).

But tactical UAVs configured for high endurance typically achieve endurance at the expense of speed and range, thus limiting the spectrum of situations in which they can be deployed.

Historically, however, attempts at airborne recovery of aircraft have met with little, if any, success.

However, even these moderate successes failed to solve the major problems associated with traditional trapeze- or arm-based airborne recovery, in which the recovered aircraft's weight must be transitioned from its own lift to the mother ship.

The transition typically happens close to the mother ship, due to the length of the recovery device, requiring the difficult connection to be made as the deployed aircraft transitions from “clean” air, to a turbulent wake and boundary layer surrounding the mother ship and finally to dead air where it cannot create sufficient lift for flight.

These transitions through different types of air make it very difficult to control the aircraft being recovered.

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